Thermoformed structural composites

A thermoformed structural-composite construct made by a process comprising the steps of:

• providing a first material having a first melting pointing, a first thermal mass, a first thermal energy density, a first thermal-energy gradient, and a first structural integrity,
• providing a second material having a second melting pointing, a second thermal mass, a second thermal energy density, a second thermal-energy gradient, and a second structural integrity,
• combining under compression between a first matched die and a second matched die to create pressure and heat applied to said first and second materials, said combination uses the differential between said first and second melting points, thermal-mass, thermal-energy-densities, thermal-energy gradients and structural integrities in the individual near-melt-point range vis-a-vis pressure-heat ratio for first said material but does not approach the melting point for the second material;
• producing a third composite material thermoformed from the merged compression of said first material with said second material, said third composite material thermoformed without distinct shear planes, and
• configuring the third composite material for a predetermined use.